STEMME S12 User Manual

DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: 
CHAPTERPAGE 335
MAINTENANCE MANUAL STEMME S12
3.6 FLIGHT CONTROL INSTRUMENTS, PITOT STATIC SYSTEM
Instruments: See Equipment List.
CAUTION
For modications sections 3.8 and 9 must be respected.
Pitot pressure, static pressure and total energy compensation are measured by means of a
multi-purpose probe in the nose-cone. Its orices are plumbed to the instrument panel through
the nose-cone sliding tube.
NOTICE
Some instruments, e. g. Bohli-diaphragm-type rate-of-climb indicator, need additional static ports
for proper operation at the widest area of the forward fuselage. These additional static ports are
installed only, if they were required for instrumentation at time of delivery.
All hose lines of the pitot-static system are equipped with a water separator/lter in the front
cockpit area below the instrument panel.

STEMME S12 Specifications

General

Brand	STEMME
Model	S12
Category	Aircrafts
Language	English